SAE ARP 1281 : 2002
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR
Superseded date
29-02-2024
Superseded by
Published date
12-09-2002
Publisher
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1 Scope
1.1 Purpose
1.2 Product Classification
1.3 Field of Application
2 References
2.1 Applicable Documents
2.2 Definitions and Abbreviations
3 Technical Requirements
3.1 General
3.2 Design
3.3 Processes, Construction/Assembly Requirements
3.4 Performance
3.5 Installation/Maintenance Requirements
3.6 Documentation
4 Quality Assurance Provisions
4.1 General
4.2 Test Requirements
4.3 Classification of Tests
4.4 Test Procedures
4.5 Test Conditions
4.6 Acceptance Test Methods
4.7 Preproduction Test Methods
4.8 Qualification Test Methods
4.9 Test Reports, Design Changes and Approval Data
4.10 Preproduction and Qualification Test Failures
5 Preparation For Delivery
5.1 Preservation For Delivery
5.2 Packing
5.3 Marking of Shipment
6 Notes
Appendix A Technical Notes and Comments
Figure
Tables
This aerospace recommended practice provides a framework and suggested procedures or values for requirements for the design, performance, and test of hydraulically powered servoactuators for use in aircraft flight control systems.
| Committee |
A-6B1
|
| DocumentType |
Revision
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| ISO 8625-1:2018 | Aerospace — Fluid systems — Vocabulary — Part 1: General terms and definitions related to pressure |
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| SAE ARP 4925 : 2014 | AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |
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| SAE AMS 2419 : 2015 | PLATING, CADMIUM-TITANIUM |
| MIL-DTL-5015 Revision H:2000 | CONNECTORS, ELECTRICAL, CIRCULAR THREADED, AN TYPE - GENERAL SPECIFICATION FOR |
| SAE AS 4716 : 2011 | GLAND DESIGN, O-RING AND OTHER SEALS |
| MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
| SAE AMS A 21180 : 2011 | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| SAE ARP 926 : 1997 | FAULT/FAILURE ANALYSIS PROCEDURE |
| SAE AS 8976 : 2012 | BEARINGS, PLAIN, SELF-ALIGNING, ALL METAL, GENERAL SPECIFICATION FOR |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-PRF-6083 Revision G:2013 | HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| SAE AMS QQ C 320 : 2000 | CHROMIUM PLATING (ELECTRODEPOSITED) |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-PRF-46170 Revision E:2013 | HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544 |
| NASM21244:2014 | NUT, CASTELLATED, HEXAGON, COUNTERBORED ASSEMBLED WASHER, 450 DEGREES F, FOR SELF-RETAINING BOLTS |
| NASM33588:2010 | NUT, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR |
| SAE AS 7949 : 2004 | BEARINGS, BALL, AIRFRAME, ANTIFRICTION, GENERAL STANDARD |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-STD-2073-1 Revision E:2008 | STANDARD PRACTICE FOR MILITARY PACKAGING |
| NASM83050:2013 | BOLT, SELF-RETAINING, IMPEDANCE TYPE |
| SAE AS 5169 : 2009 | FITTING, PORT PLUG AND BLEEDER |
| MIL-HDBK-831 Revision A:2013 | PREPARATION OF TEST REPORTS |
| SAE AS 5440 : 2011 | HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
| SAE AMS 2426E : 2013 | COATING, CADMIUM VACUUM DEPOSITION |
| NASM25027:2012 | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| MIL-PRF-131 Revision K:2005 | BARRIER MATERIALS, WATERVAPORPROOF, GREASEPROOF, FLEXIBLE, HEAT-SEALABLE |
| MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| SAE AS 6038 : 2011 | BEARINGS, BALL, BELLCRANK, ANTIFRICTION, AIRFRAME |
| SAE ARP 4493 : 2013 | AEROSPACE - DIRECT DRIVE SERVOVALVES |
| NASM3369:2013 | BOLT, SELF-RETAINING, POSITIVE LOCKING, CRES, 90 KSI FSU, 63 KSI FTU, HEXAGON SLOTTED HEAD, 450 DEGREES F AND 650 DEGREES F |
| MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
| NASM33540:2003 | SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR |
| ASME Y14.24 : 2012 | TYPES AND APPLICATIONS OF ENGINEERING DRAWINGS - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| SAE AMS S 13165 : 2007 | SHOT PEENING OF METAL PARTS |
| ASTM D 1974 : 1998 | Standard Practice for Methods of Closing, Sealing, and Reinforcing Fiberboard Boxes |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AMS STD 2175 : 1998 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| SAE J 2470 : 2009 | Hydraulic Fluid Power—Valves—Method for Assessing the Lock Sensitivity to Contaminants<br> |
| NASM20995:2012 | WIRE, SAFETY OR LOCK |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| SAE AS 39901 : 2012 | BEARINGS, ROLLER, NEEDLE, AIRFRAME, ANTIFRICTION, INCH |
| MIL-STD-882 Revision E:2012 | System Safety |
| SAE AS 6039 : 2009 | BEARINGS, BALL, ROD END, DOUBLE ROW, SELF-ALIGNING |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| NASM33602:2011 | BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR |
| SAE ARP 4945 : 2013 | AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
| MIL-PRF-22191 Revision F:2008 | Barrier Materials, Transparent, Flexible, Heat-Sealable |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| SAE AMS 2406 : 2015 | PLATING, CHROMIUM, HARD DEPOSIT |
| ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
| MS21343 Base Document:1971 | BOSS SPACING HYDRAULIC DESIGN STANDARD FOR |
| SAE AS 8775 : 1998 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
| SAE AS 4088 : 2011 | AEROSPACE ROD SCRAPER GLAND DESIGN STANDARD |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS |
| SAE AS 1241 : 2016 | FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| SAE AS 33649 : 2000 | BOSSES, FLUID CONNECTION, INTERNAL STRAIGHT THREAD |
| NASM24665:2016 | PIN, COTTER (SPLIT) |
| SAE AMS 2403 : 2015 | PLATING, NICKEL, GENERAL PURPOSE |
| SAE AMS F 7190 : 2016 | FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
| SAE AS 1290 : 2011 | GRAPHIC SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS |
| MIL-HDBK-838 Base Document:1997 | LUBRICATION OF MILITARY EQUIPMENT |
| SAE AS 4059F : 2013 | AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS |
| AN6204 Revision L:2013 | Valve, Hydraulic Bleeder |
| SAE ARP 4386 : 2010 | TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES |
| MIL-STD-1839 Revision D:2010 | STANDARD PRACTICE CALIBRATION AND MEASUREMENT REQUIREMENTS |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| MIL C 26482 : G | CONNECTOR, ELECTRICAL (CIRCULAR, MINIATURE, QUICK DISCONNECT, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS, GENERAL SPECIFICATION FOR |
| MIL-HDBK-470 Revision A:1997 | Designing and Developing Maintainable Products and Systems, Volume I |
| SAE AS 4941 : 2015 | AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
| SAE ARP 598 : 2016 | AEROSPACE MICROSCOPIC SIZING AND COUNTING OF PARTICULATE CONTAMINATION FOR FLUID POWER SYSTEMS |
| SAE AMS C 8837 : 2015 | COATING, CADMIUM (VACUUM DEPOSITED) |
| SAE ARP 1383 : 2013 | AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS |
| NASM21224:2014 | NUT, SELF-LOCKING, CASTELLATED, HEXAGON, COUNTERBORED, ASSEMBLED WASHER, 250 DEGREES F, NON-METALLIC INSERT (FOR SELF-RETAINING BOLTS) |
| NASM15981:2010 | FASTENERS, EXTERNALLY THREADED, SELF-LOCKING DESIGN AND USAGE LIMITATIONS FOR |
| ASTM B 381 : 2013 : REDLINE | SPECIFICATION FOR TITANIUM AND TITANIUM ALLOY FORGINGS |
| MIL-C-11796 Revision C:1986 | CORROSION PREVENTIVE COMPOUND, PETROLATUM, HOT APPLICATION |
| SAE ARP 490 : 2008 | ELECTROHYDRAULIC SERVOVALVES |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| MIL-PRF-8805 Revision G:2016 | SWITCHES AND SWITCH ASSEMBLIES, SENSITIVE, SNAP ACTION (BASIC, LIMIT, PUSH BUTTON AND TOGGLE SWITCHES), GENERAL SPECIFICATION FOR |
| A-A-1898 Revision D:2012 | CUSHIONING MATERIAL, CELLULOSIC, PACKAGING |
| SAE AIR 4922A : 2015 | PRIMARY FLIGHT CONTROL HYDRAULIC ACTUATION SYSTEM INTERFACE DEFINITION |
| SAE AIR 4066 : 2017 | AEROSPACE FLUID POWER - MATERIALS AND CHARACTERISTICS OF FLIGHT CONTROL SERVOACTUATORS OF VARIOUS AIRCRAFT |
| NAS847:2012 | CAPS AND PLUGS, PROTECTIVE, DUST AND MOISTURE SEAL |
| MIL-STD-961 Revision E:2003 | DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT |
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